ES2166234A1 - Un sistema de modificacion de las propiedades de rigidez/amortiguacion de uniones estructurales. - Google Patents
Un sistema de modificacion de las propiedades de rigidez/amortiguacion de uniones estructurales.Info
- Publication number
- ES2166234A1 ES2166234A1 ES009802421A ES9802421A ES2166234A1 ES 2166234 A1 ES2166234 A1 ES 2166234A1 ES 009802421 A ES009802421 A ES 009802421A ES 9802421 A ES9802421 A ES 9802421A ES 2166234 A1 ES2166234 A1 ES 2166234A1
- Authority
- ES
- Spain
- Prior art keywords
- coupled
- structures
- components
- rigidity
- modification
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000013016 damping Methods 0.000 title abstract 2
- 230000004048 modification Effects 0.000 title abstract 2
- 238000012986 modification Methods 0.000 title abstract 2
- 230000000903 blocking effect Effects 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
- B64G1/641—Interstage or payload connectors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F3/00—Spring units consisting of several springs, e.g. for obtaining a desired spring characteristic
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
- B64G1/641—Interstage or payload connectors
- B64G1/6425—Interstage or payload connectors arrangements for damping vibrations
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F7/00—Vibration-dampers; Shock-absorbers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/002—Launch systems
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T403/00—Joints and connections
- Y10T403/50—Bridged by diverse connector
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T403/00—Joints and connections
- Y10T403/59—Manually releaseable latch type
- Y10T403/591—Manually releaseable latch type having operating mechanism
- Y10T403/593—Remotely actuated
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T74/00—Machine element or mechanism
- Y10T74/21—Elements
- Y10T74/2121—Flywheel, motion smoothing-type
- Y10T74/2132—Structural detail, e.g., fiber, held by magnet, etc.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Laminated Bodies (AREA)
- Connection Of Plates (AREA)
- Road Paving Structures (AREA)
- Mutual Connection Of Rods And Tubes (AREA)
- Buildings Adapted To Withstand Abnormal External Influences (AREA)
- Joining Of Building Structures In Genera (AREA)
- Bridges Or Land Bridges (AREA)
- Body Structure For Vehicles (AREA)
- Rod-Shaped Construction Members (AREA)
Abstract
Un sistema de modificación de las propiedades de rigidez/amortiguación de uniones estructurales. Comprende al menos una estructura intermedia (3), para recibir, a uno y otro lado, sendas estructuras (1, 2) a acoplar, medios de bloqueo liberables (6), para inmovilizar, en condición acoplada, dichas dos estructuras a acoplar y dicha estructura intermedia; un primero y un segundo conjuntos de elementos biestables (7, 8), siendo las características de resistencia estructural de los elementos del primero diferentes de las de los del, segundo conjunto; estando los elementos del primer conjunto conectados interiormente a una de dichas estructuras a acoplar y a dicha estructura intermedia; estando los elementos del segundo conjunto conectados interiormente a una y otra de dichas estructuras a acoplar; encontrándose dichos elementos biestables en condición inestable cuando todas las citadas estructuras están acopladas juntas. La invención es aplicable al campo de los vehículos espaciales.
Priority Applications (10)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES009802421A ES2166234B1 (es) | 1998-11-18 | 1998-11-18 | Un sistema de modificacion de las propiedades de rigidez/amortiguacion de uniones estructurales. |
US09/334,141 US6305871B1 (en) | 1998-11-18 | 1999-06-15 | System for the modification of the rigidity and damping properties of structural joints |
CN99109839A CN1107615C (zh) | 1998-11-18 | 1999-07-16 | 一种用于改变结构连接件刚性/阻尼特性的*** |
JP11227724A JP2000154667A (ja) | 1998-11-18 | 1999-08-11 | 構造継手の剛性/減衰特性を改変するためのシステム |
EP99500146A EP1002717B1 (en) | 1998-11-18 | 1999-08-17 | A system for the modification of the rigidity/damping properties of structural joints |
DE69912070T DE69912070T2 (de) | 1998-11-18 | 1999-08-17 | Ein System zur Änderung der Steifheits/Dämpfungseigenschaften von Strukturverbindungen |
AT99500146T ATE252017T1 (de) | 1998-11-18 | 1999-08-17 | Ein system zur änderung der steifheits/dämpfungseigenschaften von strukturverbindungen |
RU99118173/11A RU2237601C2 (ru) | 1998-11-18 | 1999-08-19 | Система для изменения жесткости/демпфирующих свойств силовых соединений |
CA002287066A CA2287066A1 (en) | 1998-11-18 | 1999-10-21 | A system for the modification of the rigidity/damping properties of structural joints |
UA99116265A UA61950C2 (en) | 1998-11-18 | 1999-11-17 | System for modification of rigidity/damping properties of structural joints |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES009802421A ES2166234B1 (es) | 1998-11-18 | 1998-11-18 | Un sistema de modificacion de las propiedades de rigidez/amortiguacion de uniones estructurales. |
Publications (2)
Publication Number | Publication Date |
---|---|
ES2166234A1 true ES2166234A1 (es) | 2002-04-01 |
ES2166234B1 ES2166234B1 (es) | 2003-02-16 |
Family
ID=8305834
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES009802421A Expired - Fee Related ES2166234B1 (es) | 1998-11-18 | 1998-11-18 | Un sistema de modificacion de las propiedades de rigidez/amortiguacion de uniones estructurales. |
Country Status (10)
Country | Link |
---|---|
US (1) | US6305871B1 (es) |
EP (1) | EP1002717B1 (es) |
JP (1) | JP2000154667A (es) |
CN (1) | CN1107615C (es) |
AT (1) | ATE252017T1 (es) |
CA (1) | CA2287066A1 (es) |
DE (1) | DE69912070T2 (es) |
ES (1) | ES2166234B1 (es) |
RU (1) | RU2237601C2 (es) |
UA (1) | UA61950C2 (es) |
Families Citing this family (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SE515850C2 (sv) * | 2000-09-18 | 2001-10-15 | Saab Ericsson Space Ab | Anordning och metod vid en rymdfarkost |
GB2372976B (en) * | 2000-09-18 | 2004-07-07 | Saab Ericsson Space Ab | An Adaptor for a Spacecraft |
JP4339796B2 (ja) * | 2002-12-04 | 2009-10-07 | エーアーデーエセ カサ エスパシオ,ソシエダ リミタダ | 減衰装置 |
US7222823B2 (en) * | 2004-07-06 | 2007-05-29 | Ata Engineering, Inc. | Payload adapter |
US20060145016A1 (en) * | 2004-12-30 | 2006-07-06 | The Boeing Company | Mating of spacecraft components using shape memory materials |
US7748663B1 (en) * | 2005-05-24 | 2010-07-06 | Lockheed Martin Corporation | Launch vehicle stage integration device |
US7866607B2 (en) * | 2006-12-21 | 2011-01-11 | Intelsat | Piggyback satellite payload arrangement, a device for and method of attaching a piggyback satellite payload and adapter to be used for a piggyback satellite payload arrangement for launching the piggyback satellite |
US7905453B2 (en) * | 2006-12-21 | 2011-03-15 | Intelsat | Piggyback equipment panel payload arrangement, a device for and method of attaching a hosted secondary piggyback payload and adapter to be used for a piggyback secondary payload arrangement for launching the piggyback equipment panel secondary |
WO2014176423A1 (en) * | 2013-04-24 | 2014-10-30 | Marquette University | Variable stiffness actuator with large range of stiffness |
US10190537B2 (en) | 2013-07-02 | 2019-01-29 | Mra Systems, Inc. | Engine and band clamp |
CN104058103A (zh) * | 2014-06-27 | 2014-09-24 | 北京空间飞行器总体设计部 | 一种用于航天器柔性充气展开结构的刚柔连接结构 |
CN106864775A (zh) * | 2015-12-11 | 2017-06-20 | 天津航天瑞莱科技有限公司 | 一种航天器有效载荷减冲击装置 |
CA3020920C (en) | 2016-04-14 | 2023-10-31 | Marquette University | Variable stiffness series elastic actuator |
CN108638593A (zh) * | 2018-03-09 | 2018-10-12 | 北京宇航***工程研究所 | 一种蜂窝阻尼颗粒冲击减缓装置 |
CN109693810B (zh) * | 2018-12-29 | 2022-04-26 | 西北工业大学 | 一种用于空间碎片清理的纳星结构 |
CN109823576B (zh) * | 2019-02-20 | 2020-11-24 | 上海卫星工程研究所 | 用于行星着陆器的承载连接结构 |
CN111619831B (zh) * | 2020-04-29 | 2021-11-16 | 航天东方红卫星有限公司 | 一种连杆式星箭分离机构 |
CN112249364A (zh) * | 2020-10-28 | 2021-01-22 | 哈尔滨工业大学 | 小卫星的结构***、小卫星及组装小卫星的方法 |
CN113152708A (zh) * | 2021-02-10 | 2021-07-23 | 国机集团科学技术研究院有限公司 | 以水平抗震为主的振震双控控制策略 |
CN113415440B (zh) * | 2021-07-20 | 2022-06-17 | 哈尔滨工业大学 | 一种快速展开支撑装置 |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3529417A (en) * | 1967-11-16 | 1970-09-22 | Trw Inc | Fluid pressure actuated linear force generating means |
JPH03148400A (ja) * | 1989-11-02 | 1991-06-25 | Natl Space Dev Agency Japan<Nasda> | 衛星とロケットおよびアポジ・キック・エンジンとの結合/分離方法 |
US5244170A (en) * | 1991-10-15 | 1993-09-14 | General Dynamics Corporation, Space Systems Division | Passive nonlinear interface strut (PNIS) |
US5352061A (en) * | 1993-01-05 | 1994-10-04 | Honeywell Inc. | Anti-rotation ring joint |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3346929A (en) * | 1966-03-04 | 1967-10-17 | James E Webb | Latching mechanism |
US3458217A (en) * | 1966-11-25 | 1969-07-29 | Joseph D Pride Jr | Tubular coupling having low profile band segments with means for preventing relative rotation |
US3505925A (en) * | 1967-10-16 | 1970-04-14 | Mc Donnell Douglas Corp | Structure release system |
US3633456A (en) * | 1969-07-03 | 1972-01-11 | Mc Donnell Douglas Corp | Power-actuated separation system |
US3564564A (en) * | 1969-11-21 | 1971-02-16 | Nasa | Latching mechanism |
US3737117A (en) * | 1971-07-06 | 1973-06-05 | Nasa | Docking structure for spacecraft |
FR2516893A1 (fr) * | 1981-11-26 | 1983-05-27 | Aerospatiale | Systeme permettant le maintien temporaire et la liberation de deux parties, plus particulierement dans le domaine spatial |
FR2648199B1 (fr) | 1989-06-09 | 1991-09-27 | Aerospatiale | Dispositif de liaison temporaire, notamment pour appendice de satellite artificiel, et procede de liberation d'une telle liaison |
FR2664338B1 (fr) | 1990-07-04 | 1992-10-23 | Aerospatiale | Dispositif de liaison entre deux objets par plusieurs points de fixation. |
FR2735099B1 (fr) * | 1995-06-06 | 1997-08-29 | Aerospatiale | Dispositif adaptateur basculant pour l'emport de plusieurs charges utiles sur un meme lanceur. |
ES2120338B1 (es) | 1995-10-16 | 1999-05-01 | Const Aeronauticas Sa | Sistema de fijacion y separacion para satelites. |
US5961078A (en) * | 1997-06-27 | 1999-10-05 | Mcdonnell Douglas Corporation | Passive axial vibration isolation system for a spacecraft launch vehicle |
ES2131476B1 (es) | 1997-09-26 | 2000-03-01 | Const Aeronauticas Sa | Sistema de fijacion y separacion de satelites. |
-
1998
- 1998-11-18 ES ES009802421A patent/ES2166234B1/es not_active Expired - Fee Related
-
1999
- 1999-06-15 US US09/334,141 patent/US6305871B1/en not_active Expired - Fee Related
- 1999-07-16 CN CN99109839A patent/CN1107615C/zh not_active Expired - Fee Related
- 1999-08-11 JP JP11227724A patent/JP2000154667A/ja not_active Abandoned
- 1999-08-17 DE DE69912070T patent/DE69912070T2/de not_active Expired - Fee Related
- 1999-08-17 AT AT99500146T patent/ATE252017T1/de not_active IP Right Cessation
- 1999-08-17 EP EP99500146A patent/EP1002717B1/en not_active Expired - Lifetime
- 1999-08-19 RU RU99118173/11A patent/RU2237601C2/ru not_active IP Right Cessation
- 1999-10-21 CA CA002287066A patent/CA2287066A1/en not_active Abandoned
- 1999-11-17 UA UA99116265A patent/UA61950C2/uk unknown
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3529417A (en) * | 1967-11-16 | 1970-09-22 | Trw Inc | Fluid pressure actuated linear force generating means |
JPH03148400A (ja) * | 1989-11-02 | 1991-06-25 | Natl Space Dev Agency Japan<Nasda> | 衛星とロケットおよびアポジ・キック・エンジンとの結合/分離方法 |
US5244170A (en) * | 1991-10-15 | 1993-09-14 | General Dynamics Corporation, Space Systems Division | Passive nonlinear interface strut (PNIS) |
US5352061A (en) * | 1993-01-05 | 1994-10-04 | Honeywell Inc. | Anti-rotation ring joint |
Also Published As
Publication number | Publication date |
---|---|
EP1002717B1 (en) | 2003-10-15 |
CA2287066A1 (en) | 2000-05-18 |
CN1107615C (zh) | 2003-05-07 |
EP1002717A3 (en) | 2000-10-11 |
DE69912070D1 (de) | 2003-11-20 |
EP1002717A2 (en) | 2000-05-24 |
DE69912070T2 (de) | 2004-08-05 |
CN1253898A (zh) | 2000-05-24 |
RU2237601C2 (ru) | 2004-10-10 |
UA61950C2 (en) | 2003-12-15 |
ATE252017T1 (de) | 2003-11-15 |
JP2000154667A (ja) | 2000-06-06 |
ES2166234B1 (es) | 2003-02-16 |
US6305871B1 (en) | 2001-10-23 |
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